درباره ما
NACA-TN-3677
Investigation of lateral control near the stall analysis for required longitudinal trim characteristics and discussion of design variables
Year: 1956
Abstract: It has been recognized for some time, and shown quantitatively by the results of flight tests, that low-speed lateral control of airplanes may be insured by a simple limitation of the maximum elevator deflection so that the maximum angle of attack maintainable is that which will still allow satisfactory lateral control characteristics. However, this procedure places severe requirements on the longitudinal trim characteristics quate for the range of power settings and center-of-gravity locations encountered in flight. The purpose of this report is to provide the analytical means by which designers may estimate the elevator deflection required to trim in steady longitudinal flight and to demonstrate in a quantitative manner the effects on longitudinal trim of changes in some of the more important design parameters.
Show full item record
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:01:37Z | |
| date available | 2017-09-04T17:01:37Z | |
| date copyright | 01/01/1956 | |
| date issued | 1956 | |
| identifier other | BXNUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/125125 | |
| description abstract | It has been recognized for some time, and shown quantitatively by the results of flight tests, that low-speed lateral control of airplanes may be insured by a simple limitation of the maximum elevator deflection so that the maximum angle of attack maintainable is that which will still allow satisfactory lateral control characteristics. However, this procedure places severe requirements on the longitudinal trim characteristics quate for the range of power settings and center-of-gravity locations encountered in flight. The purpose of this report is to provide the analytical means by which designers may estimate the elevator deflection required to trim in steady longitudinal flight and to demonstrate in a quantitative manner the effects on longitudinal trim of changes in some of the more important design parameters. | |
| language | English | |
| title | NACA-TN-3677 | num |
| title | Investigation of lateral control near the stall analysis for required longitudinal trim characteristics and discussion of design variables | en |
| type | standard | |
| page | 92 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1956 | |
| contenttype | fulltext |